Improved superconducting motor stator, aircraft superconducting motor and aircraft
The invention relates to an improved superconducting electric machine stator (1) comprising a low-temperature cooler (10) in the form of a ring, inside which superconductive windings (12) are arranged, each superconductive winding being positioned on a hybrid structure (16), the hybrid structure is...
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| creator | ABDO RACHID CURELLI ROBERTO KOHLER ADELINE |
| description | The invention relates to an improved superconducting electric machine stator (1) comprising a low-temperature cooler (10) in the form of a ring, inside which superconductive windings (12) are arranged, each superconductive winding being positioned on a hybrid structure (16), the hybrid structure is formed from at least a stack of an iron element (16a) and an element (16b) made of a material having high thermal conductivity, such as a special ceramic, such as sapphire, copper, diamond or aluminum. Thus, it is possible to obtain an optimized ratio between the cooling capacity of the superconducting winding (12) and the weight of the stator (1), which is particularly advantageous in the case of an aircraft superconducting electric machine comprising such a stator (1).
本发明涉及一种改进的超导电机定子(1)，其包括环形式的低温冷却器(10)，在该低温冷却器内部布置超导绕组(12)，每个超导绕组定位在混合结构(16)上，该混合结构至少由铁元素(16a)和由具有高导热性的材料(诸如特殊陶瓷(例如蓝宝石、铜、金刚石或铝))制成的元素(16b)的堆叠形成。因此，有可能获得超导绕组(12)的冷却能力与定子(1)的重量之间的优化比率，这在包括此类定子(1)的飞行器超导电机的情况下是特别有利的。 |
| format | Patent |
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本发明涉及一种改进的超导电机定子(1)，其包括环形式的低温冷却器(10)，在该低温冷却器内部布置超导绕组(12)，每个超导绕组定位在混合结构(16)上，该混合结构至少由铁元素(16a)和由具有高导热性的材料(诸如特殊陶瓷(例如蓝宝石、铜、金刚石或铝))制成的元素(16b)的堆叠形成。因此，有可能获得超导绕组(12)的冷却能力与定子(1)的重量之间的优化比率，这在包括此类定子(1)的飞行器超导电机的情况下是特别有利的。</description><language>chi ; eng</language><subject>AIRCRAFT ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER ; COSMONAUTICS ; DYNAMO-ELECTRIC MACHINES ; ELECTRICITY ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; GENERATION ; PARACHUTES ; PERFORMING OPERATIONS ; TRANSPORTING</subject><creationdate>2024</creationdate><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20240326&DB=EPODOC&CC=CN&NR=117767691A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25562,76317</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20240326&DB=EPODOC&CC=CN&NR=117767691A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>ABDO RACHID</creatorcontrib><creatorcontrib>CURELLI ROBERTO</creatorcontrib><creatorcontrib>KOHLER ADELINE</creatorcontrib><title>Improved superconducting motor stator, aircraft superconducting motor and aircraft</title><description>The invention relates to an improved superconducting electric machine stator (1) comprising a low-temperature cooler (10) in the form of a ring, inside which superconductive windings (12) are arranged, each superconductive winding being positioned on a hybrid structure (16), the hybrid structure is formed from at least a stack of an iron element (16a) and an element (16b) made of a material having high thermal conductivity, such as a special ceramic, such as sapphire, copper, diamond or aluminum. Thus, it is possible to obtain an optimized ratio between the cooling capacity of the superconducting winding (12) and the weight of the stator (1), which is particularly advantageous in the case of an aircraft superconducting electric machine comprising such a stator (1).
本发明涉及一种改进的超导电机定子(1)，其包括环形式的低温冷却器(10)，在该低温冷却器内部布置超导绕组(12)，每个超导绕组定位在混合结构(16)上，该混合结构至少由铁元素(16a)和由具有高导热性的材料(诸如特殊陶瓷(例如蓝宝石、铜、金刚石或铝))制成的元素(16b)的堆叠形成。因此，有可能获得超导绕组(12)的冷却能力与定子(1)的重量之间的优化比率，这在包括此类定子(1)的飞行器超导电机的情况下是特别有利的。</description><subject>AIRCRAFT</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>AVIATION</subject><subject>CONVERSION OR DISTRIBUTION OF ELECTRIC POWER</subject><subject>COSMONAUTICS</subject><subject>DYNAMO-ELECTRIC MACHINES</subject><subject>ELECTRICITY</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>GENERATION</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2024</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZAjyzC0oyi9LTVEoLi1ILUrOz0spTS7JzEtXyM0vyS9SKC5JBFI6ComZRclFiWklOJQl5qXAlfAwsKYl5hSn8kJpbgZFN9cQZw_d1IL8-NTigsTk1LzUknhnP0NDc3MzczNLQ0djYtQAALfiOUk</recordid><startdate>20240326</startdate><enddate>20240326</enddate><creator>ABDO RACHID</creator><creator>CURELLI ROBERTO</creator><creator>KOHLER ADELINE</creator><scope>EVB</scope></search><sort><creationdate>20240326</creationdate><title>Improved superconducting motor stator, aircraft superconducting motor and aircraft</title><author>ABDO RACHID ; CURELLI ROBERTO ; KOHLER ADELINE</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN117767691A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2024</creationdate><topic>AIRCRAFT</topic><topic>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</topic><topic>AVIATION</topic><topic>CONVERSION OR DISTRIBUTION OF ELECTRIC POWER</topic><topic>COSMONAUTICS</topic><topic>DYNAMO-ELECTRIC MACHINES</topic><topic>ELECTRICITY</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</topic><topic>GENERATION</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>ABDO RACHID</creatorcontrib><creatorcontrib>CURELLI ROBERTO</creatorcontrib><creatorcontrib>KOHLER ADELINE</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>ABDO RACHID</au><au>CURELLI ROBERTO</au><au>KOHLER ADELINE</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Improved superconducting motor stator, aircraft superconducting motor and aircraft</title><date>2024-03-26</date><risdate>2024</risdate><abstract>The invention relates to an improved superconducting electric machine stator (1) comprising a low-temperature cooler (10) in the form of a ring, inside which superconductive windings (12) are arranged, each superconductive winding being positioned on a hybrid structure (16), the hybrid structure is formed from at least a stack of an iron element (16a) and an element (16b) made of a material having high thermal conductivity, such as a special ceramic, such as sapphire, copper, diamond or aluminum. Thus, it is possible to obtain an optimized ratio between the cooling capacity of the superconducting winding (12) and the weight of the stator (1), which is particularly advantageous in the case of an aircraft superconducting electric machine comprising such a stator (1).
本发明涉及一种改进的超导电机定子(1)，其包括环形式的低温冷却器(10)，在该低温冷却器内部布置超导绕组(12)，每个超导绕组定位在混合结构(16)上，该混合结构至少由铁元素(16a)和由具有高导热性的材料(诸如特殊陶瓷(例如蓝宝石、铜、金刚石或铝))制成的元素(16b)的堆叠形成。因此，有可能获得超导绕组(12)的冷却能力与定子(1)的重量之间的优化比率，这在包括此类定子(1)的飞行器超导电机的情况下是特别有利的。</abstract><oa>free_for_read</oa></addata></record> |
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| language | chi ; eng |
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| subjects | AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION CONVERSION OR DISTRIBUTION OF ELECTRIC POWER COSMONAUTICS DYNAMO-ELECTRIC MACHINES ELECTRICITY EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GENERATION PARACHUTES PERFORMING OPERATIONS TRANSPORTING |
| title | Improved superconducting motor stator, aircraft superconducting motor and aircraft |
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